CA3085054A1 - Systemes de commande d'aeronef - Google Patents

Systemes de commande d'aeronef Download PDF

Info

Publication number
CA3085054A1
CA3085054A1 CA3085054A CA3085054A CA3085054A1 CA 3085054 A1 CA3085054 A1 CA 3085054A1 CA 3085054 A CA3085054 A CA 3085054A CA 3085054 A CA3085054 A CA 3085054A CA 3085054 A1 CA3085054 A1 CA 3085054A1
Authority
CA
Canada
Prior art keywords
control
aircraft
processing system
inceptor
input
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CA3085054A
Other languages
English (en)
Inventor
Adam Taylor
Jonathan David DRAPER
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BAE Systems PLC
Original Assignee
BAE Systems PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from GB1721529.4A external-priority patent/GB2569601B/en
Priority claimed from EP18151965.3A external-priority patent/EP3511241A1/fr
Application filed by BAE Systems PLC filed Critical BAE Systems PLC
Publication of CA3085054A1 publication Critical patent/CA3085054A1/fr
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02Initiating means
    • B64C13/04Initiating means actuated personally
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02Initiating means
    • B64C13/04Initiating means actuated personally
    • B64C13/042Initiating means actuated personally operated by hand
    • B64C13/0421Initiating means actuated personally operated by hand control sticks for primary flight controls
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42Arrangement or adaptation of brakes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/50Steerable undercarriages; Shimmy-damping

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Mechanical Control Devices (AREA)
  • Feedback Control In General (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

L'invention concerne des systèmes de commande d'aéronef permettant d'utiliser des commandes d'entrée partagées. Un même organe de pilotage peut fournir des sorties permettant de commander des commandes d'aéronef au sol et des commandes d'aéronef dans l'air afin de réduire le nombre d'organes de pilotage requis. Dans un exemple, un manche latéral permet de commander à la fois le tangage et l'orientation du train avant de l'aéronef. Une technologie d'organe de pilotage active peut être utilisée pour fournir à l'opérateur une rétroaction sur l'état du système de commande.
CA3085054A 2017-12-21 2018-11-29 Systemes de commande d'aeronef Pending CA3085054A1 (fr)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
GB1721529.4A GB2569601B (en) 2017-12-21 2017-12-21 Aircraft control systems
GB1721529.4 2017-12-21
EP18151965.3A EP3511241A1 (fr) 2018-01-16 2018-01-16 Système de commande d'un aéronef
EP18151965.3 2018-01-16
PCT/GB2018/053448 WO2019122807A1 (fr) 2017-12-21 2018-11-29 Systèmes de commande d'aéronef

Publications (1)

Publication Number Publication Date
CA3085054A1 true CA3085054A1 (fr) 2019-06-27

Family

ID=64556943

Family Applications (1)

Application Number Title Priority Date Filing Date
CA3085054A Pending CA3085054A1 (fr) 2017-12-21 2018-11-29 Systemes de commande d'aeronef

Country Status (9)

Country Link
US (1) US11174005B2 (fr)
EP (1) EP3728026B1 (fr)
JP (1) JP7005770B2 (fr)
KR (1) KR102650037B1 (fr)
CN (1) CN111556841B (fr)
CA (1) CA3085054A1 (fr)
ES (1) ES2949956T3 (fr)
MA (1) MA51273A (fr)
WO (1) WO2019122807A1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2949956T3 (es) 2017-12-21 2023-10-04 Bae Systems Plc Sistemas de control de aeronaves
US20240228022A9 (en) * 2022-10-19 2024-07-11 Lockheed Martin Corporation Mode-dependent tactile feedback profiles for an inceptor

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2621002A (en) * 1948-11-23 1952-12-09 Lockheed Aircraft Corp Steerable landing gear for airplanes
JPS5721059Y2 (fr) 1976-08-06 1982-05-07
US4420808A (en) * 1980-04-01 1983-12-13 United Technologies Corporation Multi-axis force stick, self-trimmed aircraft flight control system
US5008825A (en) * 1989-05-01 1991-04-16 Nadkarni Arun A Apparatus and methods for automatically maintaining aircraft track angle
US5412299A (en) 1993-12-21 1995-05-02 Honeywell, Inc. Variable servo loop compensation in an active hand controller
US6671588B2 (en) 2001-12-27 2003-12-30 Toyota Jidosha Kabushiki Kaisha System and method for controlling traveling direction of aircraft
JP3817591B2 (ja) 2002-05-14 2006-09-06 学校法人金沢工業大学 自動車
GB2444678B (en) 2005-08-29 2010-09-22 Borealis Tech Ltd Nosewheel control apparatus
GB2471213B (en) * 2006-08-29 2011-05-11 Borealis Tech Ltd Nosewheel control apparatus
US7840316B2 (en) 2007-12-17 2010-11-23 Honeywell International Inc. Limited authority and full authority mode fly-by-wire flight control surface actuation control system
US20090187292A1 (en) * 2008-01-17 2009-07-23 Mark Andrew Hreha Integrated pitch, roll, and yaw inceptor
EP2303610B1 (fr) * 2008-07-28 2020-01-08 Fleck Future Concepts GmbH Véhicule routier, aquatique et aérien combiné
FR2948629B1 (fr) * 2009-07-28 2011-08-19 Eurocopter France Amortissement variable de restitution haptique pour chaine cinematique de changement d'attitude de vol d'un aeronef
US9051045B2 (en) 2010-07-28 2015-06-09 Woodward Mpc, Inc. Indirect drive active control column
US8606437B2 (en) 2011-11-28 2013-12-10 Embraer S.A. Flight control system mode and method providing aircraft speed control through the usage of momentary on-off control
US20170297605A1 (en) * 2014-10-08 2017-10-19 Aeromobil, S.R.O. A directional control system for a hybrid air and ground transportation vehicle
GB2533179B (en) * 2014-12-10 2020-08-26 Airbus Operations Ltd Control method and apparatus for an aircraft when taxiing
ES2949956T3 (es) 2017-12-21 2023-10-04 Bae Systems Plc Sistemas de control de aeronaves

Also Published As

Publication number Publication date
US20200339246A1 (en) 2020-10-29
KR102650037B1 (ko) 2024-03-20
US11174005B2 (en) 2021-11-16
MA51273A (fr) 2021-05-12
CN111556841A (zh) 2020-08-18
JP7005770B2 (ja) 2022-01-24
ES2949956T3 (es) 2023-10-04
EP3728026A1 (fr) 2020-10-28
KR20200095497A (ko) 2020-08-10
CN111556841B (zh) 2024-09-10
WO2019122807A1 (fr) 2019-06-27
JP2021507846A (ja) 2021-02-25
EP3728026B1 (fr) 2023-05-31

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Legal Events

Date Code Title Description
EEER Examination request

Effective date: 20231128